View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 14760U 26039.54618608 +.00000000 +00000-0 +80537-4 0 00006
2 14760 74.0413 84.8953 0028805 249.8277 109.9778 14.37160794 01
| Epoch (UTC): | 08 February 2026 13:06:30 |
| Eccentricity: | 0.0028805 |
| inclination: | 74.0413° |
| perigee height: | 747 km |
| apogee height: | 788 km |
| right ascension of ascending node: | 84.8953° |
| argument of perigee: | 249.8277° |
| revolutions per day: | 14.37160794 |
| mean anomaly at epoch: | 109.9778° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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